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S/SC SERIESSELIG-DATABASESYMMETRICTHIN

S8023 (7.6%)

Symmetric · 8% thick · low-to-mid Re
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PROFILES8023 (7.6%)
surfacecamber line
GEOMETRY · AREA METRICS
max thickness7.6% @ 18%c
max camber0.0% @ 0%c
LE radius0.63%c
area upper / chord0.0215
area lower / chord-0.0215
area camber / chord0.0000
TE thickness0.06%c
DOWNLOAD COORDINATES

Polars

Preliminary
NeuralFoil
-0.8128-50.11193.3331.03711.671.96120ClAngle of attack (°)
Why this curve

This is a NeuralFoil prediction from the stored profile coordinates and the selected flow condition, with AeroSandbox compressibility corrections. It is not a completed OpenFOAM calculation.

Prediction error has not been calibrated for this condition. No accuracy interval is claimed.

Geometry fit: RMS error 0.01928% of chord; maximum error 0.08001%.

NeuralFoil 0.3.3 · AeroSandbox 4.2.10

Curve summary

NeuralFoil · Within -5° to 20°

Maximum lift / drag
127.3
Angle at maximum lift / drag (°)
10
Minimum Cd
0.006275
Maximum Cl
1.73
Angle at maximum Cl (°)
17
Cd at zero lift
0.006275
Cm at zero angle
1.094e-16
CFD points
SOLVER WORK0 conditions · 0 engine jobs
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